Ceramic component

ABSTRACT

A ceramic component includes a porous structure that has fibers and a coating on the fibers. A ceramic material is within pores of the porous structure. A glass or glass/ceramic material is within pores of the porous structure, and one of the ceramic material or the glass or glass/ceramic material is within internal residual porosity of the other of the ceramic material or the glass or glass/ceramic material.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a divisional of U.S. patent application Ser. No.13/251,644, filed Oct. 28, 2011.

BACKGROUND

This disclosure relates to ceramic materials. Ceramic materials areknown and used for components such as coatings, ceramic bodies andceramic matrices. For example, ceramic materials are fabricated usingtechniques such as polymer impregnation and pyrolysis, meltinfiltration, slurry infiltration, slip casting, tape casting, injectionmolding, dry pressing, isostatic pressing, hot isostatic pressing andothers. The selected processing technique controls the chemistry andmicrostructure of the ceramic material and thus can also limit thechemistry and microstructure.

SUMMARY

A ceramic component according to a non-limiting example of the presentdisclosure includes a porous structure having fibers and a coating onthe fibers. A ceramic material is located within pores of the porousstructure. A glass or glass/ceramic material is also located withinpores of the porous structure. One of the ceramic material or the glassor glass/ceramic material is within internal residual porosity of theother of the ceramic material or the glass or glass/ceramic material.

In a further embodiment of any of the foregoing embodiments, the fibersare selected from a group consisting of ceramic fibers, carbon fibers,and combinations thereof.

In a further embodiment of any of the foregoing embodiments, the coatingincludes one or more layers of carbon, boron nitride, boron carbide,silicon nitride, silicon carbide, and aluminosilicate.

In a further embodiment of any of the foregoing embodiments, the coatingis a monolayer coating.

In a further embodiment of any of the foregoing embodiments, the coatingis a multilayer coating.

A further embodiment of any of the foregoing embodiments includes theglass material, and the glass material is a silicate-based glass thatincludes at least one of boron, barium, magnesium, lithium, andaluminum.

In a further embodiment of any of the foregoing embodiments, the glassmaterial includes a silicon-containing filler.

In a further embodiment of any of the foregoing embodiments, the ceramicmaterial is selected from a group consisting of silicon carbide, siliconcarbonitride, silicon nitride, silicon oxycarbide, alumina, andcombinations thereof.

In a further embodiment of any of the foregoing embodiments, the ceramicmaterial includes a filler selected from the group consisting of siliconcarbide, aluminum nitride, boron carbide, refractory materials, boronnitride, silicon nitride, diamond and combinations thereof.

In a further embodiment of any of the foregoing embodiments, the poresare interconnected.

In a further embodiment of any of the foregoing embodiments the ceramiccomponent has a final composition, by volume percentage, of:

20-70 of the porous structure,

1-12 of the coating on the fibers,

1-75 of the ceramic material, and

a balance of the glass or glass/ceramic material and residual voidvolume, wherein the residual void volume is less than 5 volume percent.

In a further embodiment of any of the foregoing embodiments the ceramiccomponent has a final composition, by volume percentage, of:

30-50 of the porous structure,

2-5 of the coating on the fibers,

25-65 of the ceramic material, and

a balance of the glass or glass/ceramic material and the residual voidvolume.

BRIEF DESCRIPTION OF THE DRAWINGS

The various features and advantages of the disclosed examples willbecome apparent to those skilled in the art from the following detaileddescription. The drawings that accompany the detailed description can bebriefly described as follows.

FIG. 1 illustrates an example method of fabricating a ceramic component.

FIG. 2 illustrates various stages through fabrication of a ceramiccomponent.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

FIG. 1 illustrates an example method 20 of fabricating a ceramiccomponent. As will be appreciated, the method 20 permits fabrication ofceramic components having unique compositions and/or microstructuresthat are not heretofore available. Furthermore, the method 20 can beused to produce compositions and/or microstructures for the enhancementof densification, thermal conductivity or other target property incomponents such as cooled turbine engine components.

As illustrated in FIG. 1, the method 20 generally includes an initialinfiltration step 22 and further infiltration steps 24 a and 24 b. Asshown, initial infiltration step 22 includes initially partially fillingpores of a porous structure using one of a first processing technique ora second, different processing technique. If selected for initiallypartially filling the pores, the first processing technique produces afirst ceramic material in the pores. Alternatively, the secondprocessing technique produces a second ceramic material that initiallypartially fills the pores. The second ceramic material is different fromthe first ceramic material in at least one of composition,microstructure and physical property. The infiltration step 22 resultsin the intermediate formation of a preform body with residual porosity.

The term “processing technique” refers to the kind of the technique,rather than to variations between specific, but similar processes.Processing techniques differ in the way that ceramic precursors aredelivered into a green state and the formation mechanisms of the finalceramic material from the precursor(s). Thus, techniques that utilizedelivery/formation mechanisms via polymer infiltration/pyrolysis,solvent infiltration/sintering, melt infiltration/solidification, vapordeposition, dry powder/sintering, and pressure injection/sintering aredifferent processing techniques.

In addition, although some characteristics may differ between twospecific processes, such characteristics do not differentiate the twoprocesses when the methods of delivery of the precursors are the same orthe formation mechanisms are the same. For instance, one meltinfiltration technique is not different from another melt infiltrationtechnique merely because the temperatures of the infiltrations differ,nor are two polymer infiltration/pyrolysis techniques different merelybecause different polymer precursors are used. However, polymerinfiltration/pyrolysis is a different processing technique than meltinfiltration/solidification even though each includes infiltrationbecause the infiltrations utilize different precursors that form therespective final ceramic materials via different formation mechanisms,pyrolysis and solidification, respectively. Given this description, oneof ordinary skill in the art will be able to distinguish differentprocessing techniques.

In embodiments, the first and second processing techniques are selectedfrom the techniques of polymer infiltration/pyrolysis, solventinfiltration/sintering, melt infiltration/solidification, vapordeposition, dry powder/sintering, and pressure injection/sintering. Infurther examples, however, the first and second processing techniquesare not limited to these disclosed techniques and other techniques arealternatively used, assuming compatibility between the selectedtechniques with regard to delivery and formations mechanisms.

The infiltration steps 24 a and 24 b depend upon which processingtechnique is used to initially partially fill the pores of the porousstructure. In step 24 a, when the first processing technique is used toinitially partially fill the pores of the porous structure, the secondprocessing technique is performed thereafter to at least partially fillthe residual porosity with the second ceramic material. Alternatively,in step 24 b, when the second processing technique is instead used toinitially partially fill the pores of the porous structure, the firstprocessing technique is performed thereafter to at least partially fillthe residual porosity with the first ceramic material. Thus, in eitheralternative, the latter-used processing technique serves to at leastpartially backfill the residual porosity that remains within the preformbody from the earlier-used processing technique. In this regard, the twoprocessing techniques are fully compatible such that either can be theearlier-used or latter-used processing technique, to partially fill theresidual porosity and thereafter at least partially fill the residualinternal porosity such that a total void volume of the ceramic componentis less than five volume percent.

The filling of the residual porosity (at least partially) by thelatter-used processing technique increases the densification of thefinal component and can optionally be used to enhance other propertiesof the component, such as thermal conductivity or mechanical properties.In one example, the residual void volume after the latter-usedprocessing technique is less than five volume percent. In a furtherexample, the residual void volume is less than one volume percent.

In one embodiment, the first processing technique includes infiltrationwith a preceramic polymer material and a thermal treatment to convertthe preceramic polymer material to a ceramic material. For example, thepreceramic polymer material is a polycarbosilane that decomposes tosilicon carbide. In another example, the preceramic polymer is apolycarbosiloxane that decomposes into silicon oxycarbide. In stillanother example, the polymer is a polysilazane material that decomposesto silicon carbide, silicon carbonitride, silicon nitride orcombinations thereof. Additional preceramic polymers and combinations ofpreceramic polymers are also contemplated. The thermal treatment isconducted in a controlled environment with regard to at least one oftemperature, time and process gas, or in a variety of differentcontrolled environments, to control the composition of the resultingceramic material. Further, the preceramic polymer material can includefillers, such as silicon carbide, aluminum nitride, boron carbide,refractory materials, boron nitride, silicon nitride, diamond andcombinations thereof, to control the properties and/or composition ofthe resulting ceramic material.

The second processing technique includes infiltration of the residualporosity with a heated, liquid glass or glass/ceramic material (e.g.,glass transfer molding) and solidification of the liquid glass orglass/ceramic material to a solid glass or glass/ceramic material. Asused herein, the term “ceramic” refers to inorganic, non-metallicmaterials that may be crystalline, partially crystalline orsubstantially or fully amorphous. Further, the term “glass” as usedherein, refers to an amorphous or partially amorphous ceramic material.Also further, the term “glass/ceramic” as used herein is a glasscomposition that, upon proper controlled exposure to temperature, time,pressure, and environmental conditions will precipitate out one or morebeneficial crystalline ceramic phase(s) for property modification.Glass/ceramic materials are known to share many properties with bothglasses and ceramics.

In a further embodiment, the porous structure is a porous fibrousstructure. For example, the porous fibrous structure is a fabric, weave,braid, tape, two-dimensional, or three-dimensional woven or non-wovenstructure that is coated or uncoated with a protective coating. In oneexample, the porous fibrous structure includes ceramic fibers and/orcarbon fibers. In some examples, the ceramic fibers include oxide ornon-oxide ceramic fibers. In a further example, the fibers are siliconcarbide fibers. In other examples, the fibers are silicon oxycarbide,doped-silicon carbide or silicon oxycarbide and/or glass orglass/ceramic fibers. It is to be understood that the porous structuremay alternatively be another kind of porous structure that may or maynot include fibers.

In a further embodiment, the porous fibrous structure includes aprotective coating on the fibers. The protective coating includes anoxide layer, a non-oxide layer or both and can be a monolayer coating ora multilayer coating. For instance, the protective coating includes oneor more layers of carbon, boron nitride, boron carbide, silicon nitride,silicon carbide and aluminosilicate. The function of the protectivecoating may be selected to prevent degradation of the underlying fibrousstructure or to control the interactions between the fibrous structureand the void filling materials described herein.

In a further embodiment, the glass or glass/ceramic material issilicate-based. For example, the silicate-based glass or glass/ceramicincludes boron, barium, magnesium, lithium, aluminum or combinationsthereof. In a further example, the silicate-based glass or glass/ceramicadditionally includes a nucleating agent that serves to precipitatecrystalline phases from the amorphous phase with the application ofthermal treatment. In one non-limiting example, the nucleating agentincludes zirconium or a compound containing zirconium.

In a further embodiment, the selected glass or glass/ceramic materialadditionally includes a solid filler to modify the properties of theceramic component. In one example, the solid filler is a solid ceramicfiller, such as silicon carbide. In other examples, the solid filler isa silicon-containing filler, such as oxides, nitrides, borides, carbidesand combinations thereof that include silicon.

The composition with regard to the volume percentages of the porousstructure, any protective coating on the porous structure and theceramic material from the polymer infiltration/pyrolysis processingtechnique are controlled such that the residual porosity of preform bodyis within a predetermined range. As an example, the predetermined rangeis selected such that, once backfilled with the glass or glass/ceramicmaterial from the glass transfer/solidification processing technique,there is a targeted volume percentage of the glass or glass/ceramicmaterial. Thus, the method 20 can be tailored to control the volumepercentages of the ceramic and glass or glass/ceramic phases. In oneexample, the residual porosity of the preform body is no greater thanapproximately 43 volume percent.

In another example, the predetermined range is selected such that theresidual porosity in the preform body is surface connected andinterconnected. That is, the porosity is above a percolation threshold.In one example, the residual porosity is approximately 20-43 volumepercent of the preform body. The surface connection and interconnectionpermits the liquid glass or glass/ceramic material in the latter-usedprocessing technique to infiltrate through the preform body to enhancethe density of the final ceramic component. In one example, the finalceramic component has a residual void volume of less than five volumepercent, and in further examples less than one volume percent.

In another embodiment, the first processing technique is used toinitially partially fill the pores of the porous structure. Prior toperforming the second processing technique, the first processingtechnique is repeated for a selected number of cycles to control theresidual porosity to be within a predetermined range. In one example,the processing technique of infiltration with a preceramic polymer andthermal treatment to convert the polymer to ceramic material is repeatedbetween two and nine times to sequentially reduce the residual porosityto the predetermined range. When the residual porosity is within thepredetermined desired range, a second processing technique ofinfiltration with a heated, liquid glass or glass/ceramic material andsolidification is then performed to at least partially fill theremaining residual porosity.

Similarly, if the second processing technique is used to initiallypartially fill the pores of the porous structure, the second processingtechnique can be repeated for a selected number of cycles beforeperforming the first processing technique. As an example, the processingtechnique of infiltration with the heated, liquid glass or glass/ceramicmaterial and solidification is repeated before performing a secondprocessing technique of infiltration with the preceramic polymer and thethermal treatment to convert the polymer to ceramic material.

In another alternative, the first processing technique is used toinitially partially fill the pores of the porous structure and thesecond processing technique is thereafter performed to partially fillthe residual porosity. Either the first or second processing techniqueis then repeated for a selected number of cycles to at least partiallyfill any remaining porosity after the second processing technique. Auser can subsequently perform additional cycles of the first and/orsecond processing techniques to further densify or modify the propertiesof the ceramic component.

In a further example of the method 20, a preceramic polymer material isimpregnated into a porous structure that includes a fibrous sheet thatis coated or uncoated with a protective coating. For instance, thefibrous sheet is a fabric, weave, tape or braid. Alternatively, theporous structure can be another type of two-dimensional fiber structureor three-dimensional woven or non-woven structure. The fibrous sheet isthen divided into plies and the plies are stacked in a desirableorientation relative to one another. The stack is then compressed, underheat, to consolidate the sheets and polymerize, rigidize or cure thepreceramic polymer. Alternatively, the stacked sheets are vacuum-baggedin an autoclave process to consolidate and cure the sheets into a morecomplex geometry.

The consolidated sheets are then pyrolyzed at a suitable temperature andtime in a controlled environment to convert the preceramic polymer toceramic material and thereby form a preform body having a residualporosity. The preform body is then subjected to a ceramic glass-transfermolding process in which the body is located in a suitable molding tool.Molten glass or glass/ceramic of a selected composition is injected intothe tool cavity to infiltrate the residual porosity of the preform body.The component is then cooled to solidify the glass or glass/ceramic intoa solid glass or glass/ceramic material. Optionally, an additional heattreatment is conducted to crystallize the solid glass or glass/ceramicand/or grow crystals of desired ceramic phase(s) in a controlled manner.

FIG. 2 illustrates three different stages (A), (B) and (C) in afabrication of a final ceramic component 40 according to the method 20.It is to be understood that the method 20 is not limited to fabricationof the exemplary ceramic component 40. As shown in initial stage (A), aporous structure 42 includes a plurality of fibers 44 that define openpores 46 there between. Optionally, as shown, each of the fibers 44includes a protective coating 48 of composition described hereindisposed on the outer surfaces of the fibers 44.

As shown in stage (B), the pores 46 are initially partially filled bythe first or second processing technique with a ceramic material 50 ofcomposition described herein, which thereby forms a preform body withresidual porosity 52. At least a portion of the residual porosity 52 issurface-connected, as shown schematically by dashed lines 52 a.Additionally, in one example, at least a portion of the residualporosity 52 is interconnected, as represented schematically at dashedline 52 b. The residual porosity includes residual internal porositydefined by the ceramic material 50. The residual internal porosityincludes voids, micro-cracks or other open regions that are bounded bythe ceramic material 50 and which evolve from the processing techniquethat forms the ceramic material 50.

As shown at stage (C), the latter-used processing technique at leastpartially fills the residual porosity 52 with another ceramic material54 of composition described herein that is different from the ceramicmaterial 50 in at least one of composition, microstructure or physicalproperty. Thus, the ceramic material 54 at least partially fills theresidual porosity 52 within the ceramic material 50.

In a further example, the ceramic material 50 has a coefficient ofthermal conductivity that is greater than the coefficient of thermalconductivity of the other ceramic material 54. Thus, the ceramicmaterial 50 is selected for enhancement of thermal conductivity of theceramic component 40, while the other ceramic material 54 can beselected to enhance other properties of the ceramic component 40, suchas thermal resistance, dimensional stability and corrosion resistance.

The ceramic materials 50 and 54 are alternatively transposed in themicrostructure such that the regions shown as being occupied by theceramic material 54 are occupied by the ceramic material 50, and viceversa. In this example, the ceramic material 54 is initially infiltratedinto the pores 46 of the porous structure 42 to partially fill the pores46, leaving a residual porosity that is then later at least partiallyfilled with the ceramic material 50.

In the illustrated example, the ceramic component 40 includes a finalcomposition, by volume percentage, of:

20-70 of the porous structure 42,

1-12 of the coating 48 on the porous structure 42,

1-75 of the ceramic material 50 or 54, and

a balance of the other ceramic material 50 or 54 and residual voidvolume, wherein the residual void volume is less than 5 volume percent.

In a further example, the final composition includes:

30-50 of the porous structure 42,

2-5 of the coating 48,

25-65 of the ceramic material 50 or 54, and

a balance of the other ceramic material 50 or 54 and the residual voidvolume.

Although a combination of features is shown in the illustrated examples,not all of them need to be combined to realize the benefits of variousembodiments of this disclosure. In other words, a system designedaccording to an embodiment of this disclosure will not necessarilyinclude all of the features shown in any one of the Figures or all ofthe portions schematically shown in the Figures. Moreover, selectedfeatures of one example embodiment may be combined with selectedfeatures of other example embodiments.

The preceding description is exemplary rather than limiting in nature.Variations and modifications to the disclosed examples may becomeapparent to those skilled in the art that do not necessarily depart fromthe essence of this disclosure. The scope of legal protection given tothis disclosure can only be determined by studying the following claims.

What is claimed is:
 1. A ceramic component comprising: a porousstructure including fibers and a coating on the fibers; a ceramicmaterial within pores of the porous structure; and a glass orglass/ceramic material within pores of the porous structure, wherein oneof the ceramic material or the glass or glass/ceramic material is withininternal residual porosity of the other of the ceramic material or theglass or glass/ceramic material.
 2. The ceramic material as recited inclaim 1, wherein the fibers are selected from a group consisting ofceramic fibers, carbon fibers, and combinations thereof.
 3. The ceramicmaterial as recited in claim 1, wherein the coating includes one or morelayers of carbon, boron nitride, boron carbide, silicon nitride, siliconcarbide, and aluminosilicate.
 4. The ceramic material as recited inclaim 1, wherein the coating is a monolayer coating.
 5. The ceramicmaterial as recited in claim 1, wherein the coating is a multilayercoating.
 6. The ceramic material as recited in claim 1, including theglass material, and the glass material is a silicate-based glass thatincludes at least one of boron, barium, magnesium, lithium, andaluminum.
 7. The ceramic material as recited in claim 6, wherein theglass material includes a silicon-containing filler.
 8. The ceramiccomponent as recited in claim 1, wherein the ceramic material isselected from a group consisting of silicon carbide, siliconcarbonitride, silicon nitride, silicon oxycarbide, alumina, andcombinations thereof.
 9. The ceramic component as recited in claim 8,wherein the ceramic material includes a filler selected from the groupconsisting of silicon carbide, aluminum nitride, boron carbide,refractory materials, boron nitride, silicon nitride, diamond andcombinations thereof.
 10. The ceramic component as recited in claim 1,wherein the pores are interconnected.
 11. The ceramic component asrecited in claim 1, having a final composition, by volume percentage,of: 20-70 of the porous structure, 1-12 of the coating on the fibers,1-75 of the ceramic material, and a balance of the glass orglass/ceramic material and residual void volume, wherein the residualvoid volume is less than 5 volume percent.
 12. The ceramic component asrecited in claim 11, having a final composition, by volume percentage,of: 30-50 of the porous structure, 2-5 of the coating on the fibers,25-65 of the ceramic material, and a balance of the glass orglass/ceramic material and the residual void volume